Boeing 737-222

Service difficulty reports · 657

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '737222'
  ORDER BY difficulty_date DESC"

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SDR P2EA99146Stringer · crackedSJO - DURING C-CHECK, ON THE EXTERIOR FUSELAGE BETWEEN BS 986 AND BS 1016, STRINGER 21L WAS FOUND WITH SEVERAL SMALL CRACKS. REPAIRED FUSELAGE NR 21 LEFT STRINGER SECTION BETWEEN BS 973 AND BS 1016 DUE TO CRACKS PER SRM 53-10-3, FIGURE 1. (M)Apr 2, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Longeron/StringerSDR P2EA99142Stringer · crackedSJO - DURING C-CHECK, THE FUSELAGE BETWEEN BS 986 AND BS 1016, STRINGER 23L WAS FOUND WITH SEVERAL SMALL CRACKS. REPAIRED FUSELAGE STRINGER 23 LEFT BETWEEN BS 970 AND BS 1016 DUE TO CRACKS PER SRM 53-10-3, FIGURE 1. FABRICATED STRINGER AND SPLICE PER SRM 51-Apr 2, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Longeron/StringerSDR P2EA99152Skin · delaminatedSJO - DURING C-CHECK, THE LEFT WING OUTBOARD TE FLAP SKIN WAS FOUND WITH DELAMINATION. REPAIRED OUTBOARD FLIPPER FLAP P/N 65-71930-1 PER EO COO-CMP-3-57-214-99 DATED APR 5, 1999. (M)Mar 31, 1999 · N603DJ · Boeing 737222 · Trailing Edge FlapsSDR P2EA99145Skin · delaminationSJO - DURING C-CHECK, THE LEFT WING UPPER SURFACE TRAILING EDGE FIXED PANEL BETWEEN WBL 100 AND WBL 180 WAS FOUND WITH DELAMINATION. REPAIRED WING FIXED PANEL P/N 65-50820-141 PER EO COO-CMP-3-57-216-99, DATED APR 7, 1999. (M)Mar 31, 1999 · N603DJ · Boeing 737222 · Wing, Plate/SkinSDR P2EA99140Skin · delaminatedSJO - DURING C-CHECK, THE LEFT WING NR 1 SPOILER WAS FOUND WITH DELAMINATION. REPAIRED SPOILER P/N 65-46451-25 PER EO COO-CMP-3-57-213-99, DATED APR 5, 1999. ASSIGNED SERIAL NUMBER VAG-6 TO SPOILER PART NR 65-46451-25. REPLACED UPPER AND LOWER SKIN AND HONEMar 31, 1999 · N603DJ · Boeing 737222 · SpoilersSDR P2EA99139Skin · delaminationSJO - DURING C-CHECK, THE RIGHT WING TRAILING EDGE FIXED PANEL BETWEEN WBL 114 AND WBL 157 WAS FOUND WITH DELAMINATION. REPAIRED WING FIXED PANEL P/N 65-50826-142 PER EO COO-CMP-3-57-215-99, DATED 4-6-99. (M)Mar 31, 1999 · N603DJ · Boeing 737222 · Wing, Plate/SkinSDR P2EA99134Skin · crackedSJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR OUTER SKIN, HANDLE CUTOUT WAS FOUND WITH A CRACK. REPAIRED FCC DOOR OUTER SKIN HANDLE CUTOUT SECTION BETWEEN BS 461 AND BS 474 FROM NR 3 BEAM TO NR 4 BEAM DUE TO CRACK IAW SRM 52-00-3, FIG 6. (M)Mar 31, 1999 · N603DJ · Boeing 737222 · Cargo/Baggage DoorsSDR P2EA99182Skin · corrodedSJO - DURING C-CHECK, THE EXTERIOR FUSELAGE FROM BS 947 TO BS 967 AND BETWEEN STRINGER 20 RIGHT AND STRINGER 19 RIGHT WAS FOUND WITH BULGED SKIN. REPLACED AND FABRICATED FUSELAGE SKIN PANEL FROM BS 908 TO BS 1016, BETWEEN STRINGER 14 RIGHT AND STRINGER 20 RIGMar 29, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99174Skin · corrodedSJO - DURING C-CHECK, THE FUSELAGE SKIN AT BS 907 AFT WAS FOUND WITH CORROSION, MATERIAL LOSS MORE THAN 15 PERCENT BETWEEN STRINGER 21 LEFT AND 22 LEFT. REPLACED FUSELAGE SKIN PANEL BETWEEN BS 907 AND BS 1016, FROM STRINGER 20 TO STRINGER 25 LEFT SIDE DUE TO Mar 29, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99172Bulkhead Web · corrodedSJO - DURING C-CHECK, AT THE AFT CARGO COMPARTMENT AFT PRESSURE BULKHEAD, BS 1016, BETWEEN STRINGERS 26R AND 27R, PRESSURE BULKHEAD WEB SECTION WAS FOUND WITH CORROSION. REPAIRED PRESSURE BULKHEAD WEB SECTION AT BS 1016, BETWEEN STRINGER 26 LEFT AND STRINGER Mar 28, 1999 · N603DJ · Boeing 737222 · Fuselage Main, BulkheadSDR P2EA99155Beam · crackedSJO - DURING C-CHECK, THE AFT CARGO COMPARTMENT DOOR LOWER CROSSBEAM WEB AND OUTER CHORD WAS FOUND CRACKED AT THE AFT LOWER SECTION, DISCOVERED DURING COMPLIANCE WITH VANGUARD EO 993752A002. REPAIRED LOWER CROSSBEAM AND OUTER CHORD IN THE AFT LOWER SECTION OFMar 28, 1999 · N603DJ · Boeing 737222 · Cargo/Baggage DoorsSDR P2EA99138Bellcrank · wornSJO - DURING C-CHECK, THE LEFT WING OUTBOARD FLAP INBOARD TRACK MOVABLE FAIRING SUPPORT WAS FOUND WITH PLAY AND THE LINK WAS FOUND WITH WEAR. PERFORMED BLENDOUT REPAIR AT LEFT WING OUTBOARD FLAP INBOARD TRACK BELLCRANK SECTION DUE TO WEAR PER COOPESA EO COO-3Mar 28, 1999 · N603DJ · Boeing 737222 · Trailing Edge Flap Control SystemSDR P2EA99135Skin · corrodedSJO - DURING C-CHECK, THE FUSELAGE FROM BS 996 TO BS 1016 ON STRINGERS 6 RT AND 7 RT OUTER SKIN WAS FOUND BULGED. REPAIRED FUSELAGE SKIN BUTT JOINT EXTERNAL SKIN FROM BS 1008 TO BS 1016, BETWEEN STRINGERS 5 RT AND 4RT PER SRM 53-30-3, FIGURE 28, SHEETS 1, 2, Mar 28, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99181Skin · crackedSJO - DURING C-CHECK, CRACKS WERE FOUND ON THE FUSELAGE OUTER SKIN AT BS 219.8, WL 218 AND AT BS 211.8, WL 228 RIGHT SIDE. REPAIRED FUSELAGE SKIN SECTIONS FROM BS 216.8 TO BS 223, BETWEEN WL212 AND WL 224 RIGHT SIDE, AND FROM BS 207L8 TO BS 215.8 BETWEEN WL 2Mar 27, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99176Beam · crackedSJO - DURING C-CHECK, LEFT WHEEL WELL, BS 663.75, LBL 68, STRINGER 18A SHEAR BEAM SECTION WAS FOUND WITH A CRACK. REPAIRED LEFT FUSELAGE STRINGER 18A SHEAR BEAM SECTION AT BS 663.75, BL 68, WL 200 DUE TO CRACK PER 737-53-1066, SECTION III, PART II, REVISION 3Mar 27, 1999 · N603DJ · Boeing 737222 · Fuselage Miscellaneous StructureSDR P2EA99175Beam · crackedSJO - DURING C-CHECK, RIGHT WHEEL WELL, BS 663.75, RBL 68, STRINGER 18A SHEAR BEAM SECTION WAS FOUND WITH A CRACK. REPAIRED RIGHT FUSELAGE STRINGER 18A SHEAR BEAM SECTION AT BS 663.75, RBL 68, WL 200 DUE TO CRACK PER SB 737-53-1066, SECTION III, PART III, REVMar 27, 1999 · N603DJ · Boeing 737222 · Fuselage Miscellaneous StructureSDR P2EA99173Skin · crackedSJO - DURING C-CHECK, THE EXTERIOR FUSELAGE SKIN WAS FOUND WITH CRACKS BETWEEN STRINGER 14 LEFT AND STRINGER 16 LEFT AT BS 727A. REPAIRED THE FUSELAGE SKIN SECTION BETWEEN BS 727 AND BS 727B PLUS 15 INCH, FROM STRINGER 14 TO STRINGER 20 LEFT SIDE DUE TO CRACKMar 27, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99167Frame · crackedSJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR CUTOUT, STRINGER 20 RIGHT, DOORWAY FRAME WAS FOUND WITH A CRACK AT BS 440. REPLACED THE FORWARD CARGO COMPARTMENT DOOR CUTOUT FRAME AT BS 440, BETWEEN STRINGERS 17 RIGHT AND 28 RIGHT PER SB 737-53-1051,Mar 27, 1999 · N603DJ · Boeing 737222 · Fuselage Miscellaneous StructureSDR P2EA99159Skin · damagedSJO - DURING C-CHECK, THE RIGHT WING UPPER SKIN AT WBL 157 WAS FOUND WITH SPOTFACE DAMAGE. REPAIRED THE RIGHT WING UPPER SKIN SURFACE AT WBL 157, BETWEEN STRINGER 4 AND STRINGER 6 DUE TO EXISTING SPOTFACES PER COOPESA EO COO-3-57-208-99, DATED APR 2, 1999 ANDMar 27, 1999 · N603DJ · Boeing 737222 · Wing, Plate/SkinSDR P2EA99158Beam · corrodedSJO - DURING C-CHECK, THE AFT CARGO COMPARTMENT DOOR, FORWARD NR 5 STOP SECTION AND WEB WERE FOUND CRACKED. REPAIRED AFT CARGO COMPARTMENT DOOR LOWER CROSSBEAM FORWARD SECTION DUE TO CRACK PER SB 737-52-1079, SECTION III, PAR II, REVISION 5 DATED MAY 16, 1996Mar 27, 1999 · N603DJ · Boeing 737222 · Cargo/Baggage DoorsSDR P2EA99154Casting · damagedSJO - DURING C-CHECK, THE FORWARD CARGO COMPARTMENT DOOR OUTER HANDLE CASTING WAS FOUND WITH A HOLE IN IT. REPLACED THE FORWARD CARGO COMPARTMENT DOOR OUTER HANDLE CASTING PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. PERFORMED REMOVAL AND INSTALLATION OF THE CARGMar 27, 1999 · N603DJ · Boeing 737222 · Cargo/Baggage DoorsSDR P2EA99148Skin · corrodedSJO - DURING C-CHECK, THE FUSELAGE BS 178 UPPER SECTION LBL 8 OUTER SKIN WAS FOUND WITH MISSING MATERIAL. REPAIRED FUSELAGE UPPER SKIN SECTION BS 178, LBL 8 PER COOPESA EO COO-3-53-210-99, DATED APR 5, 1999. (M)Mar 27, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99144Beam · crackedSJO - DURING C-CHECK, THE FORWARD CARGO DOOR NR 5 BEAM WEB WAS FOUND WITH A CRACK. REPAIRED FORWARD CARGO COMPARTMENT DOOR NR 5 BEAM WEB AFT SECTION DUE TO CRACK PER SB 737-52-1100, SECTION III, FIGURE 6, REVISION 2, DATED MAR 31, 1994. (M)Mar 27, 1999 · N603DJ · Boeing 737222 · Passenger/Crew DoorsSDR P2EA99137Stiffener · crackedSJO - DURING C-CHECK, A/C DISTRIBUTION BAY, BS 540, RBL 23, WL 208, STIFFENER WAS FOUND WITH A CRACK. REPLACED FUSELAGE STIFFENER AT BS 540, RBL 23 BETWEEN WL 208 AND WL 152 DUE TO CRACK PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Mar 27, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Longeron/StringerSDR P2EA99136Door · crackedSJO - DURING C-CHECK, THE LEFT MAIN LANDING DOOR SHOCK STRUTS DOOR WS FOUND WITH A CRACK. REPAIRED LEFT MLG SHOCK STRUT DOOR BETWEEN BS 698.80 AND BS 694.80 DUE TO CRACK IAW COOPESA EO C00-3057-219-99 DATED APR 6, 1999 AND BOEING FAX C00-SJO-99-0447RR DATED AMar 27, 1999 · N603DJ · Boeing 737222 · Landing Gear DoorsSDR P2EA99127Keel Beam · corrodedSJO - DURING Q-CHECK, A SECTION OF THE KEEL BEAM AT BS 630, RBL 5 WAS FOUND WITH CORROSION. THE AREA WAS REPAIRED AS PER COOPESA EO C00-3-53-176-99 AND BOEING FAX NR COO-SJO-0384RR. (M)Mar 13, 1999 · N208AU · Boeing 737222 · Fuselage Main, KeelSDR P2EA99141Floorbeam · corrodedSJO - DURING C-CHECK, IN THE PASSENGER CABIN, FORWARD LAVATORY AREA BS 294.5, LBL 55, FLOORBEAM WAS FOUND CORRODED. REPAIRED FLOORBEAM UPPER CHORD BS 294.5 BETWEEN LBL 59 AND RBL 59 DUE TO CORROSION PER SRM 51-10-1 FIGURE 5, AND UPPER CHORD SPLICED AT RBL 24 Mar 3, 1999 · N603DJ · Boeing 737222 · Fuselage Main, Floor BeamSDR P2EA99078Data Plate · out of adjustDFW - FLT 815 - UPON GEAR SELECTED DOWN, RECEIVED INTERMITTENT GEAR WARNING GEAR UNSAFE (RED) LIGHT. SAME THING DURING TAXI IN. REMOVED COVER FOR NLG DOWN LOCK SENSOR. FOUND DATA PLATE RESTING AGAINST SENSOR TERMINAL BLOCK. VERIFIED REPORTED CONDITION BY RMar 2, 1999 · N603DJ · Boeing 737222 · Placards and MarkingsSDR P2EA99091Bolt · wornSJO - DURING Q-CHECK, THE NR 2 ENGINE, AFT MOUNT ATTACH BOLT, WAS FOUND WITH WEAR. NR 2 ENGINE AFT MOUNT ATTACH BOLT REPLACED IAW MM 71-21-11. (M)Mar 1, 1999 · N208AU · Boeing 737222 · Engine Mount SectionSDR P2EA99077Gcu · failedMDW - FLT 703 - ABORTED TAKEOFF AT 103 KNOTS DUE TO FAILURE OF THE NR 1 GENERATOR BUS TRANSFER SYSTEM. THE NR 4 MAIN TIRE BLEW OUT DURING ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT IAW MM 24-21-81. OPS CHECK NORMAL. REMOVED AND REPLAFeb 28, 1999 · N209US · Boeing 737222 · AC RegulatorSDR P2EA99083Skin · damagedSJO - DURING Q-CHECK, A SKIN REPAIR AT BS 500A, STRINGER 26R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3, FIGURE 16. (M)Feb 26, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99101Panel · delaminatedSJO - DURING Q-CHECK, THE RIGHT WING FIXED TRAILING EDGE PANEL, P/N 65-70947-24 WAS FOUND DELAMINATED. THE PANEL WAS REPAIRED IW EO NR COO-CMP-3-57-159-99. (M)Feb 25, 1999 · N208AU · Boeing 737222 · Wing, Plate/SkinSDR P2EA99100Skin · delaminatedSJO - DURING Q-CHECK, THE LEFT WING NR 2 TRAILING EDGE SLAT WAS FOUND WITH DELAMINATION. THE SLAT WAS REPAIRED IAW EO NR COO-CMP-3-57-149-99. (M)Feb 25, 1999 · N208AU · Boeing 737222 · Trailing Edge FlapsSDR P2EA99111Skin · delaminatedSJO - DURIGN Q-CHECK RIGHT AILERON WAS FOUND WITH DELAMINATION. AILERON WAS REPAIRED AS PER COOPESA NR COO-CMP-3-57-151-99. (M)Feb 24, 1999 · N208AU · Boeing 737222 · AileronsSDR P2EA99097Skin · delaminatedSJO - DURING Q-CHECK, FLIGHT SPOILER NR 3 WAS FOUND WITH DELAMINATION. FLIGHT SPOILER REPAIRED AS PER COOPESA EO NR COO-CMP-3-57-150-00. (M)Feb 24, 1999 · N208AU · Boeing 737222 · SpoilersSDR P2EA99092Bolts · wornSJO - DURING Q-CHECK, NR 2 ENGINE, FORWARD MOUNT THRUST LINKS ATTACH BOLTS FOUND WITH WEAR. REPLACED ATTACH BOLTS AS PER MM 71-20-11. (M)Feb 24, 1999 · N208AU · Boeing 737222 · Engine Mount SectionSDR P2EA99089Bolt · wornSJO - DURING Q-CHECK, ENGINE NR 1 FORWARD MOUNT THRUST LINK ATTACH BOLTS FOUND WITH WEAR. BOLTS REPLACED AS PER MM 71-20-11. (M)Feb 24, 1999 · N208AU · Boeing 737222 · Engine Mount SectionSDR P2EA99118Mechanism · corrodedSJO - DURING Q-CHECK, THE R2 DOOR HANDLE MECHANISM HOUSING WAS FOUND WITH CORROSION AT THE LOWER TORQUE TUBE POSITION. REWORKED BEARING BORE AND MOUNTING HOLES AS PER OHM 52-46-05. (M)Feb 23, 1999 · N208AU · Boeing 737222 · Service DoorsSDR P2EA99117Bearing · corrodedSJO - DURING Q-CHECK, THE R1 DOOR WAS FOUND WITH CORROSION ON THE UPPER TORQUE TUBE BEARING POSITION. THE BEARING BORE AND MOUNTING HOLES WERE REWORKED AS PER OHM 52-46-06. (M)Feb 23, 1999 · N208AU · Boeing 737222 · Service DoorsSDR P2EA99106Skin · delaminatedSJO - DURING Q-CHECK, DELAMINATION WAS FOUND ON THE LEFT AILERON. THE AILERON WAS REPAIRED PER COOPESA EO COO-CMP-3-57-127-99. (M)Feb 23, 1999 · N208AU · Boeing 737222 · AileronsSDR P2EA99084Bulkhead Chord · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE BS 178 PRESSURE BULKHEAD, FORWARD SIDE, LOWER HORIZONTAL CHORD. CRACK WAS REPAIRED IAW SRM 51-40-4 FIGURE 1. (M)Feb 23, 1999 · N208AU · Boeing 737222 · Fuselage Main, BulkheadSDR P2EA99126Support · wornSJO - DURING Q-CHECK, THE NR 1 ENGINE THRUST REVERSER, RIGHT ACTUATOR SUPPORT WAS WORN TO LIMITS. THE ACTUATOR SUPPORT WAS REPLACED IAW SRM 51-10-1. (M)Feb 22, 1999 · N208AU · Boeing 737222 · Engine Thrust ReverserSDR P2EA99107Skin · crackedSJO - DURING Q-CHECK, LFEC DETECTED A CRACK IN A FASTENER HOLE AT BS 492.4, BETWEEN STRINGERS 23 AND 24 RIGHT. THE AREA WAS REPAIRED AS PER COOPESA EO NR COO-2-53-157-99 AND BOEING FAX NR COO-SJO-99-0319. (M)Feb 22, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99125Firewall · wornSJO - DURING Q-CHECK, THE NR 2 ENGINE PYLON FORWARD FIREWALL WAS FOUND WORN. THE FIREWALL PANEL WAS REPAIRED AS PER COOPESA EO NR 3-54-189-99 AND BOEING FAX COO-SJO-99-0389. (M)Feb 21, 1999 · N208AU · Boeing 737222 · Nacelle/Pylon, Bulkhead/FirewallSDR P2EA99124Intercostal · corrodedSJO - DURING Q-CHECK, A STIFFENER AND INTERCOSTAL IN THE E/E COMPARTMENT BETWEEN BS 294.5 AND BS 312 AT STRINGER WERE FOUND WITH CORROSION. THE INTERCOSTAL AND STIFFENER WERE REPLACED AS PER SRM 51-30-2. (M)Feb 21, 1999 · N208AU · Boeing 737222 · Fuselage Miscellaneous StructureSDR P2EA99099Bulkhead Web · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE WEB OF THE PRESSURE BULKHEAD AT BS 294.5 BETWEEN STRINGER 27 AND 28 RT IN THE E/E COMPARTMENT. WEB SECTION WAS REPAIRED IAW EO NR COO-3-53-146-99 AND BOEING FAX NR COO-SJO-99-0293. (M)Feb 21, 1999 · N208AU · Boeing 737222 · Fuselage Main, BulkheadSDR P2EA99085Rib · crackedSJO - DURING Q-CHECK, A RIB WAS FOUND CRACKED IN THE RIGHT WING INTERNAL AREA AT WS 505 UPPER FLANGE. THE CRACK WAS REPAIRED IAW SRM 57-10-7 FIG 1. (M)Feb 21, 1999 · N208AU · Boeing 737222 · Wing, Rib/BulkheadSDR P2EA99123Frame · crackedSJO - DURING Q-CHECK, THE BS 685 RIGHT FRAME FITTING WAS FOUND CRACKED. THE CRACK WAS REPAIRED AS PER BOEING FAX NR COO-SJO-99-0388RR AND COOPESA EO NR COO-3-53-155-99. (M)Feb 20, 1999 · N208AU · Boeing 737222 · Fuselage Main, FrameSDR P2EA99119Skin · crackedSJO - DURING Q-CHECK, THE L1 DOOR CUT OUT LOWER AFT CORNER OUTER SKIN WAS FOUND CRACKED. THE SKIN WAS REPAIRED FROM BS 322 TO 355 IAW SB 53-1083 REV 3, PART IV AND DRAWING NR 65C27253. (M)Feb 20, 1999 · N208AU · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99098Floorbeam · crackedSJO - DURING Q-CHECK, THE UPPER FLANGE OF THE FLOORBEAM AT BS 668.75, LBL 25 WAS FOUND CRACKED. REPAIRED FLOORBEAM AS PER COOPESA EO NR COO-3-53-154-99 AND BOEING FAX NR COO-SJO-98-0993RR. (M)Feb 20, 1999 · N208AU · Boeing 737222 · Fuselage Main, Floor Beam
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